Remote-control system of stratospheric airship and control method thereof

Through the four-level remote control system and multi-mode design, the complexity and fault tolerance problems of the stratospheric airship remote control system are solved, and efficient and reliable airship control is achieved, adapting to complex environments and fault conditions.

CN106828860AActive Publication Date: 2017-06-13BEIJING TIANHENG CHANGYING TECH CO LTD
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Patent Information

Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
BEIJING TIANHENG CHANGYING TECH CO LTD
Filing Date
2017-03-01
Publication Date
2017-06-13

AI Technical Summary

⚠Technical Problem

Due to the complex flight environment and high energy demand, the existing stratospheric airship remote control system is prone to insufficient energy supply or system failure. Moreover, the traditional single centralized control method is inefficient and has poor fault tolerance, and cannot meet the complex airship control needs.

⚗Method used

A four-level remote control system is designed, including the decision-making layer, planning layer, execution layer and perception layer. It uses intelligent decision-making module, multimedia information integration module and recording and playback module to realize dynamic switching of flight mode and motor drive control, providing Standard mode, combined posture adjustment mode and failure mode, real-time monitoring and data collection to improve control efficiency and fault tolerance.

🎯Benefits of technology

The airship's environmental adaptability and fault tolerance are significantly improved, the long-term control effect is enhanced, the control device is simplified and the control efficiency and reliability are improved.

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Abstract

The invention relates to a remote-control system of a stratospheric airship and a control method thereof. The control system is divided to four levels: a decision-making level for executing the selection and switch of a remote-control flight mode according to the actual working state data, and sending a corresponding mode command; a planning level for dynamically planning and generating an airship motor drive command according to the mode command sent by the decision-making level; an executing level for realizing the drive control to an airship motor according to the motor drive command of the planning level; and a perceiving level for finishing the real-time monitoring and data collection of the airship working state, and providing the original data of the airship working state to the decision-making level. The four-level control system architecture design of the control system is capable of simplifying the control device, improving the control efficiency, and fundamentally solving the problems of the function, efficiency and reliability of the near space airship ground and airborne control system.
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